/* nag_mesh2d_front (d06acc) Example Program.
*
* Copyright 2014 Numerical Algorithms Group.
*
* Mark 7, 2001.
* Mark 7b revised, 2004.
*/
#include <math.h>
#include <stdio.h>
#include <nag.h>
#include <nag_stdlib.h>
#include <nagd06.h>
/* Structure to allow data to be passed onto */
/* the nag_mesh2d_bound (d06bac) user-supplied function fbnd */
struct user
{
/* details of the double NACA0012 and the circle around it */
double x0, y0, x1, y1, radius;
};
#ifdef __cplusplus
extern "C" {
#endif
static double NAG_CALL fbnd(Integer, double, double, Nag_Comm *);
#ifdef __cplusplus
}
#endif
#define EDGE(I, J) edge[3*((J) -1)+(I) -1]
#define LINED(I, J) lined[4*((J) -1)+(I) -1]
#define CONN(I, J) conn[3*((J) -1)+(I) -1]
#define COOR(I, J) coor[2*((J) -1)+(I) -1]
#define COORCH(I, J) coorch[2*((J) -1)+(I) -1]
#define COORUS(I, J) coorus[2*((J) -1)+(I) -1]
int main(void)
{
const Integer nus = 1, nvmax = 2000, nedmx = 200, nvint = 40;
struct user geom_Naca;
double dnvint, radius, x0, x1, y0, y1;
Integer exit_status = 0, i, itrace, j, k, l, ncomp, nedge, nelt,
nlines;
Integer nv, nvb, nvint2, reftk;
char pmesh[2];
double *coor = 0, *coorch = 0, *coorus = 0, *rate = 0, *weight = 0;
Integer *conn = 0, *edge = 0, *lcomp = 0, *lined = 0, *nlcomp = 0;
NagError fail;
Nag_Comm comm;
INIT_FAIL(fail);
printf(" nag_mesh2d_front (d06acc) Example Program Results\n\n");
/* Skip heading in data file */
scanf("%*[^\n] ");
/* Initialise boundary mesh inputs: the number of lines and */
/* the number of characteristic points of the boundary mesh */
scanf("%ld", &nlines);
scanf("%*[^\n] ");
/* Allocate memory */
if (!(coor = NAG_ALLOC(2*nvmax, double)) ||
!(coorch = NAG_ALLOC(2*nlines, double)) ||
!(coorus = NAG_ALLOC(2*nus, double)) ||
!(rate = NAG_ALLOC(nlines, double)) ||
!(weight = NAG_ALLOC(nvint, double)) ||
!(conn = NAG_ALLOC(3*(2*nvmax+5), Integer)) ||
!(edge = NAG_ALLOC(3*nedmx, Integer)) ||
!(lined = NAG_ALLOC(4*nlines, Integer)) ||
!(lcomp = NAG_ALLOC(nlines, Integer)))
{
printf("Allocation failure\n");
exit_status = -1;
goto END;
}
/* The double NACA0012 and the circle around it */
for (j = 1; j <= nlines; ++j) scanf("%lf", &COORCH(1, j));
scanf("%*[^\n] ");
for (j = 1; j <= nlines; ++j) scanf("%lf", &COORCH(2, j));
scanf("%*[^\n] ");
/* The lines of the boundary mesh */
for (j = 1; j <= nlines; ++j)
{
for (i = 1; i <= 4; ++i) scanf("%ld", &LINED(i, j));
scanf("%lf", &rate[j-1]);
}
scanf("%*[^\n] ");
/* The number of connected components to */
/* the boundary and their information */
scanf("%ld", &ncomp);
scanf("%*[^\n] ");
/* Allocate memory */
if (!(nlcomp = NAG_ALLOC(ncomp, Integer)))
{
printf("Allocation failure\n");
exit_status = -1;
goto END;
}
j = 0;
for (i = 0; i < ncomp; ++i)
{
scanf("%ld", &nlcomp[i]);
scanf("%*[^\n] ");
l = j + abs(nlcomp[i]);
for (k = j; k < l; ++k) scanf("%ld", &lcomp[k]);
scanf("%*[^\n] ");
j += abs(nlcomp[i]);
}
scanf(" ' %1s '%*[^\n]", pmesh);
/* Data passed to the user-supplied function */
x0 = 1.5;
y0 = 0.0;
radius = 4.5;
x1 = 0.8;
y1 = -0.3;
comm.p = (Pointer)&geom_Naca;
geom_Naca.x0 = x0;
geom_Naca.y0 = y0;
geom_Naca.radius = radius;
geom_Naca.x1 = x1;
geom_Naca.y1 = y1;
itrace = 0;
/* Call to the 2D boundary mesh generator */
/* nag_mesh2d_bound (d06bac).
* Generates a boundary mesh
*/
nag_mesh2d_bound(nlines, coorch, lined, fbnd, coorus, nus, rate, ncomp,
nlcomp, lcomp, nvmax, nedmx, &nvb, coor, &nedge, edge,
itrace, 0, &comm, &fail);
if (fail.code == NE_NOERROR)
{
if (pmesh[0] == 'N')
{
printf(" Boundary mesh characteristics\n");
printf(" nvb =%6ld\n", nvb);
printf(" nedge =%6ld\n", nedge);
}
else if (pmesh[0] == 'Y')
{
/* Output the mesh to view it using the NAG Graphics Library */
printf(" %10ld %10ld\n", nvb, nedge);
for (i = 1; i <= nvb; ++i)
printf(" %4ld %15.6e %15.6e \n",
i, COOR(1, i), COOR(2, i));
for (i = 1; i <= nedge; ++i)
printf(" %4ld %4ld %4ld %4ld\n",
i, EDGE(1, i), EDGE(2, i), EDGE(3, i));
}
else
{
printf("Problem with the printing option Y or N\n");
exit_status = -1;
goto END;
}
}
else
{
printf("Error from nag_mesh2d_bound (d06bac).\n%s\n",
fail.message);
exit_status = 1;
goto END;
}
/* Initialise mesh control parameters */
itrace = 0;
/* Generation of interior vertices */
/* for the wake of the first NACA */
nvint2 = nvint/2;
dnvint = 5.0/(nvint2 + 1.0);
for (i = 1; i <= nvint2; ++i)
{
reftk = nvb + i;
COOR(1, reftk) = i*dnvint + 1.0;
COOR(2, reftk) = 0.0;
weight[i-1] = 0.05;
}
/* for the wake of the second one */
dnvint = 4.19/(nvint2 + 1.0);
for (i = nvint2+1; i <= nvint; ++i)
{
reftk = nvb + i;
COOR(1, reftk) = (i - nvint2)*dnvint + 1.8;
COOR(2, reftk) = -0.3;
weight[i-1] = 0.05;
}
/* Call to the 2D Advancing front mesh generator */
/* nag_mesh2d_front (d06acc).
* Generates a two-dimensional mesh using an Advancing-front
* method
*/
nag_mesh2d_front(nvb, nvint, nvmax, nedge, edge, &nv, &nelt,
coor, conn, weight, itrace, 0, &fail);
if (fail.code == NE_NOERROR)
{
if (pmesh[0] == 'N')
{
printf(" Complete mesh characteristics\n");
printf(" nv =%6ld\n", nv);
printf(" nelt =%6ld\n", nelt);
}
else if (pmesh[0] == 'Y')
{
/* Output the mesh to view it using the NAG Graphics Library */
printf(" %10ld %10ld\n", nv, nelt);
for (i = 1; i <= nv; ++i)
printf(" %15.6e %15.6e\n", COOR(1, i), COOR(2, i));
reftk = 0;
for (k = 1; k <= nelt; ++k)
printf(" %10ld%10ld%10ld%10ld\n",
CONN(1, k), CONN(2, k), CONN(3, k), reftk);
}
else
{
printf("Problem with the printing option Y or N\n");
exit_status = -1;
goto END;
}
}
else
{
printf("Error from nag_mesh2d_front (d06acc).\n%s\n",
fail.message);
exit_status = 1;
goto END;
}
END:
NAG_FREE(coor);
NAG_FREE(coorch);
NAG_FREE(coorus);
NAG_FREE(rate);
NAG_FREE(weight);
NAG_FREE(conn);
NAG_FREE(edge);
NAG_FREE(lcomp);
NAG_FREE(lined);
NAG_FREE(nlcomp);
return exit_status;
}
double NAG_CALL fbnd(Integer i, double x, double y, Nag_Comm *pcomm)
{
double ret_val;
double c, radius, x0, x1, y0, y1;
struct user *geom_Naca = (struct user *) pcomm->p;
x0 = geom_Naca->x0;
y0 = geom_Naca->y0;
radius = geom_Naca->radius;
x1 = geom_Naca->x1;
y1 = geom_Naca->y1;
ret_val = 0.0;
switch (i)
{
case 1:
/* upper NACA0012 wing beginning at the origin */
c = 1.008930411365;
ret_val = 0.6*(0.2969*sqrt(c*x) - 0.126*(c*x) - 0.3516*pow(c*x, 2.0)
+ 0.2843*pow(c*x, 3.0) - 0.1015*pow(c*x, 4.0)) - c*y;
break;
case 2:
/* lower NACA0012 wing beginning at the origin */
c = 1.008930411365;
ret_val = 0.6*(0.2969*sqrt(c*x) - 0.126*(c*x) - 0.3516*pow(c*x, 2.0)
+ 0.2843*pow(c*x, 3.0) - 0.1015*pow(c*x, 4.0)) + c*y;
break;
case 3:
/* the circle around the double NACA */
ret_val = (x-x0)*(x-x0) + (y-y0)*(y-y0) - radius*radius;
break;
case 4:
/* upper NACA0012 wing beginning at (X1;Y1) */
c = 1.008930411365;
ret_val = 0.6*(0.2969*sqrt(c*(x-x1)) - 0.126*c*(x-x1) -
0.3516*pow(c*(x-x1), 2.0) + 0.2843*pow(c*(x-x1), 3.0) -
0.1015*pow(c*(x-x1), 4.0)) - c*(y-y1);
break;
case 5:
/* lower NACA0012 wing beginning at (X1;Y1) */
c = 1.008930411365;
ret_val = 0.6*(0.2969*sqrt(c*(x-x1)) - 0.126*(c*(x-x1)) -
0.3516*pow(c*(x-x1), 2.0) + 0.2843*pow(c*(x-x1), 3.0) -
0.1015*pow(c*(x-x1), 4.0)) + c*(y-y1);
break;
}
return ret_val;
}